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contributor authorLee, Junsik
contributor authorRen, Zhong
contributor authorHaegele, Jacob
contributor authorPotts, Geoffrey
contributor authorSik Jin, Jae
contributor authorLigrani, Phil
contributor authorFox, Michael D.
contributor authorMoon, Hee
date accessioned2017-05-09T01:13:35Z
date available2017-05-09T01:13:35Z
date issued2014
identifier issn0889-504X
identifier otherturbo_136_05_051013.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/156595
description abstractData which illustrate the effects of jettotarget plate distance and Reynolds number on the heat transfer from an array of jets impinging on a flat plate are presented. Considered are Reynolds numbers Rej ranging from 8200 to 52,000 with isentropic jet Mach numbers of approximately 0.1 to 0.2. Jettotarget plate distances Z of 1.5D, 3.0D, 5.0D, and 8.0D are employed, where D is the impingement hole diameter. Streamwise and spanwise hole spacings are 8D. Local and spatiallyaveraged Nusselt numbers show strong dependence on the impingement jet Reynolds number for all situations examined. Experimental results also illustrate the dependence of local Nusselt numbers on normalized jettotarget plate distance, especially for smaller values of this quantity. The observed variations are partially due to accumulating crossflows produced as the jets advect downstream, as well as the interactions of the vortex structures, which initially form around the jets and then impact and interact as they advect away from stagnation points along the impingement target surface. The highest spatiallyaveraged Nusselt numbers are present for Z/D = 3.0 for Rej of 8200, 20,900, and 30,000. When Rej = 52,000, spatiallyaveraged Nusselt numbers increase as Z/D decreases, with the highest value present at Z/D = 1.5.
publisherThe American Society of Mechanical Engineers (ASME)
titleEffects of Jet To Target Plate Distance and Reynolds Number on Jet Array Impingement Heat Transfer
typeJournal Paper
journal volume136
journal issue5
journal titleJournal of Turbomachinery
identifier doi10.1115/1.4025228
journal fristpage51013
journal lastpage51013
identifier eissn1528-8900
treeJournal of Turbomachinery:;2014:;volume( 136 ):;issue: 005
contenttypeFulltext


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